Integrated Flight Deck Cockpit Reference Guide Diamond DA40/40F
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ABNORMAL OPERATIONS ANNUNCIATIONS & ALERTS INDEX
Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0369.13 or later for the Diamond DA40 and DA40F. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000.
WARNINGS, CAUTIONS, & NOTES NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared.
RECORD OF REVISIONS Part Number 190-00324-00 Initial Release 190-00324-01 Reformat of manual Added NAV/COM volume levels Added Flight Timer Added extended range fuel tanks Changed NAV1 and NAV2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposite sides 190-00324-02 Added WX 500 Stormscope Added XM Weather Added ADF/DME Added bearing pointers Added fixed pitch propeller engine parameters Updated fixed pitch propeller engine parameters.
RECORD OF REVISIONS Revision Date of Revision Affected Pages A 5/07 i-Index-4 RR-2 Description Production Release Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
TABLE OF CONTENTS Section 1: System Overview ......................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-5 MFD Softkeys .......................................................... 1-8 MFD Page Groups ................................................... 1-9 Vertical Navigation .............................................. 1-10 Backlighting ......
TABLE OF CONTENTS Approach .................................................................. 6-30 Go Around/Missed Approach ..................................... 6-32 6.6 AFCS Annunciations and Alerts ......................... 6-33 AFCS Status Alerts..................................................... 6-33 Overspeed Protection ................................................ 6-34 Section 7: Navigation........................................................ 7-1 7.1 Navigation Map Page ....................
TABLE OF CONTENTS 10.4 Traffic Information Service (TIS) ....................... 10-7 Displaying Traffic on the Traffic Map Page................... 10-7 Displaying Traffic on the Navigation Map ................... 10-7 TIS Audio Alert .......................................................... 10-7 10.5 Avidyne® TAS600 Series ...................................... 10-8 Displaying Traffic on the Traffic Map Page................... 10-8 Displaying Traffic on the Navigation Map ................... 10-8 10.
TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Pilot’s Guide (190-00592-03). 190-00324-07 Rev.
SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS 1 2 3 5 4 17 6 7 8 9 Figure 1-1 PFD/MFD Controls 18 10 14 19 24 11 15 20 25 12 16 21 26 22 27 23 28 13 MFD Only (with optional GFC 700) 1-2 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. 1 NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies.
SECTION 1 SYSTEM OVERVIEW G1000 displays a list that is too long for the display screen, a scroll bar appears along the right side of the display, indicating the availability of additional items within the selected category. Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list. 14 15 16 17 18 1-4 MENU Key – Displays a context-sensitive list of options.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON Softkey OFF ADF/DME Figure 1-2 PFD Top Level Softkeys ADF/DME ALERTS STRMSCP ALERTS Press the BACK or OFF Softkey to return to the top-level softkeys. Figure 1-3 INSET Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey.
SECTION 1 SYSTEM OVERVIEW ADF/DME DME ALERTS ALT UNIT HSI FRMT BRG1 (NAV1) BRG2 (NAV2) BRG1 (GPS) BRG2 (GPS) BRG1 (ADF) BRG2 (ADF) BRG1 (OFF) BRG2 (OFF) 360 HSI ALERTS Press the STD BARO or BACK Softkey to return to the top-level softkeys ARC HSI ALERTS ALERTS METERS IN HPA ALERTS Figure 1-4 PFD Configuration Softkeys PFD – Press to display the additional softkeys for additional configuration of the PFD. DFLTS – Press to reset default settings on the PFD.
SECTION 1 SYSTEM OVERVIEW GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF in the BRG2 Information Window. OFF – Removes the BRG2 Information Window. ALT UNIT – Displays softkeys for setting the altimeter and BARO settings to metric units: METERS – When enabled, displays altimeter in meters. IN – Press to display the BARO setting as inches of mercury. HPA – Press to display the BARO setting as hectopacals.
SECTION 1 SYSTEM OVERVIEW IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports Window. ALERTS – Press to display the Alerts Window. 1.3 MFD SOFTKEYS ENGINE – Pressing this softkey makes available the Engine Page.
SECTION 1 SYSTEM OVERVIEW STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the Navigation Map. XM LTNG (optional) – Pressing this softkey displays/ removes XM Radio lightning data on the Navigation Map. BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys. DCLTR (declutter) – Pressing this softkey removes map information in three levels.
SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION In WAAS capable installations, one of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance for a WAAS approach. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-WAAS systems. The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation.
SECTION 1 SYSTEM OVERVIEW White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical speed and deviation guidance.
SECTION 1 SYSTEM OVERVIEW 1.6 BACKLIGHTING When system power is turned off, all manual backlighting settings will return to the factory default settings. Manually adjust the backlight for the PFD and MFD: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. 2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the small FMS Knob to display the selection window. 4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key.
SECTION 1 SYSTEM OVERVIEW 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: Figure 1-12 Database Update Confirmation 1) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of the PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. 2) Apply power to the G1000 System. View the MFD power-up splash screen.
SECTION 1 SYSTEM OVERVIEW Blank Page 1-14 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 16 1 15 14 2 13 3 12 11 4 10 5 9 8 7 6 1 Traffic Annunciation 9 Flight Plan Window 2 Vspeed References 10 Barometric Minimums Box 3 Selected Heading Box 11 Annunciation Window 4 Wind Data Window 12 Selected Altitude Bug 5 Inset Map 13 Selected Course Box 6 BRG1 Information Window 14 Barometric Minimums Bug 7 DME Information Window 15 Glidesope Indicator 8 BRG2 Information Window 16 Marker Beacon Annunciation Figure 2-2 Additional PF
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Airspeed Trend Vector Actual Airspeed Vspeed References Speed Ranges (low end yellow band not displayed and other low end speed True Airspeed ranges differ on EASA Box certified aircraft) Figure 2-4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Vspeed References Vspeed References are turned on or off in the Timer/References Window.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Trend Vector Altitude Reference Box Altitude Reference Bug The end of the trend vector displays approximately what the altitude will be in six seconds if the current rate of vertical speed is maintained. Barometric Setting Box Altitude Trend Vector Current Altitude Select barometric pressure: Turn the BARO Knob to select the desired setting. Quickly enter standard pressure: 1) Press the PFD Softkey.
SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation (WAAS Only) Metric Display Display altitude in meters and barometric pressure in hectopascals: 1) Press the PFD Softkey to display the second level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to display altitude in meters. 4) Press the HPA Softkey to display the barometric setting in hectopascals. Press the IN Softkey to display the barometric setting in inches of mercury.
SECTION 2 FLIGHT INSTRUMENTS 2.4 VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach (see Figure 2-11). In systems that are WAAS enabled, the Glidepath Indicator appears at a point prior to the FAF when executing an LPV, LNAV/VNAV, or LNAV+V approach (see Figure 2-12).
SECTION 2 FLIGHT INSTRUMENTS 2.5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker 2.7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitude minimums can be set in the Timer/References Window. The altitude ranges from 0 to 16,000 feet in 10-foot increments. The minimums are reset anytime the power is cycled. Figure 2-16 Barometric Minimum Descent Altitude Settings Altimeter Figure 2-14 Marker Beacon Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled.
SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
Terminal Terminal 0.3 nm 1.0 nm 1.0 nm 2.0 nm Enroute (Oceanic if >200 nm from nearest airport) 31 nm from Destination Airport Departure 30 nm from Departure Airport 1.0 nm 0.
SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer. Press the BRG1 or BRG2 Softkey to cycle through selecting NAV1/2, GPS, or ADF for display using the corresponding pointer.
SECTION 2 FLIGHT INSTRUMENTS • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. • DR – Navigating using Dead Reckoning due to an error in the GPS solution. 2.9 WIND DATA When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”.
SECTION 2 FLIGHT INSTRUMENTS 2.10 GENERIC TIMER Figure 2-31 Timer Status Prompts Change the Generic Timer: 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. 2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.
SECTION 2 FLIGHT INSTRUMENTS Blank Page 2-14 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) The Engine Instrument Display is displayed on the left side of the MFD.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.1 DA40 ENGINE DISPLAY Pressing the ENGINE Softkey displays the EISENGINE Page as shown in Figure 3-2. Fuel used (GALLONS USED), endurance, and range (RANGE NM) are all calculated based on the last manual adjustment of the fuel remaining (GALLONS REMAIN). Measured fuel quantity has no effect on fuel calculations. Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 DA40F ENGINE DISPLAY Pressing the ENGINE Softkey displays the EISENGINE Page as shown in Figure 3-3. Fuel used (GALLONS USED), endurance, and range (RANGE NM) are all calculated based on the last manual adjustment of the fuel remaining (GALLONS REMAIN). Measured fuel quantity has no effect on fuel calculations. Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 ENGINE LEANING While viewing the EIS-ENGINE Page, press the LEAN Softkey. As the mixture is leaned, one of the cylinder’s exhaust temperature will peak. This is indicated by ‘1st’ being displayed below the first cylinder to peak. See Figure 34. The ∆ Peak temperature is the difference between the peak temperature and the present temperature. Continuing to lean the mixture will cause each cylinder to peak until the last of the cylinders peaks.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cylinder Peak Temperature Last Cylinder to Peak Indicates Difference Between Present and Peak Temperature of the Last Peaked Cylinder Figure 3-5 Leaning to Last Peak (DA40 shown) 190-00324-07 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Blank Page 3-6 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations. NAV Controls NAV Frequency Box COM Frequency Box COM Controls Figure 4-1 G1000 VHF NAV/COM Interface (PFD) 190-00324-07 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Selected COM Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Standby COM Frequency Field Tuning Box Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ‘ID’ indication appears to the left of the corresponding active NAV frequency.
SECTION 4 – NAV/COM & TRANSPONDER DME Radio (optional) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn the FMS Knobs to highlight the desired frequency. 3) Press the ENT Key to place the frequency in the standby field of the active COM. Figure 4-8 ADF/DME Tuning Window Change the DME tuning source: 1) From the tuning window, turn the large FMS Knob to highlight the desired DME source. 2) Turn the small FMS Knob to display the selection window.
SECTION 4 – NAV/COM & TRANSPONDER Standby Mode (Manual) Press the STBY Softkey. In Standby Mode, the transponder does not reply to interrogations, but new codes can be entered. STBY Mode (White Code Number and Mode) Reply Indication Figure 4-15 Reply Indication Code Selection VFR Code Selection Figure 4-12 Standby Mode Manual ON Mode Press the ON Softkey. ON Mode generates Mode A and Mode S replies, but Mode C altitude reporting is inhibited.
SECTION 4 – NAV/COM & TRANSPONDER Enter Code Using the FMS Knob 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference Window. 2) Press the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. 3) Turn the small FMS Knob to enter the first two digits. 4) Turn the large FMS Knob to place the cursor in position to change the second two digits.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transceiver Audio (COM 3 is unavailable) Transmitters (COM3 MIC is unavailable) Split COM (Unavailable) Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (ADF & DME optional, AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Outer Marker Annunciator Middle Marker Annunciator Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key.
SECTION 5 – AUDIO PANEL 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the NAV/COM radios and music. Selection scenarios are addressed in Table 5-1. 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL The GFC 700 AFCS is optional on the DA40 and DA40F. In aircraft without the GFC 700 option, refer to the operating instructions for the installed autopilot system for details. 6.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Activating the Flight Director Command Bars Pressing the FD or AP Key (when the flight director is not active) activates the flight director in default pitch/roll modes. Pushing the GA Switch or any flight director mode key activates the flight director in the respective mode(s). The flight director may be turned off by pressing the FD Key. Upon activation of the flight director, Command Bars are displayed on the PFD as a single cue.
SECTION 6 – AUTOMATIC FLIGHT CONTROL AFCS Status Box Flight director roll modes are shown on the left and pitch on the right. Armed modes are annunciated in white and active in green. Autopilot status is displayed in the center of the AFCS Status Box. 6.3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Table 6-1 lists the pitch modes with their corresponding controls and annunciations. The mode reference (shown with default measurement units) is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/ NOSE DN Keys can be used to change the pitch mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) Changing the Pitch Reference When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when the mode is activated.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Selected Altitude Capture Mode (ALTS) Selected Altitude Capture Mode arms automatically when the flight director is in Pitch Hold, Vertical Speed, Flight Level Change, or Go Around Mode. This mode is also armed automatically under Vertical Path Tracking Mode when the Selected Altitude is to be captured instead of the VNAV Target Altitude. The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 6-5 for example).
SECTION 6 – AUTOMATIC FLIGHT CONTROL If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed. To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected Altitude is reached.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode Active Vertical Selected Altitude Capture Speed Mode Armed Reference Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Figure 6-8 Vertical Speed Mode Changing the Vertical Speed Reference The Vertical Speed Reference (shown both in the AFCS Status Box and above/below the Vertical Speed Indicator) may be changed by: • Using the NOSE UP/NOSE DN Keys • By pressing the CWS Butt
SECTION 6 – AUTOMATIC FLIGHT CONTROL descent). The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Navigation Modes (VPTH, ALTV) NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The autopilot guides the aircraft back to the descent path upon release of the CWS Button. NOTE: VNAV flight director pitch modes are available only in conjunction with GPS roll modes. NOTE: The Selected Altitude takes precedence over any other vertical constraints.
SECTION 6 – AUTOMATIC FLIGHT CONTROL In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Data Box, VNAV indications (VNAV Target Altitude, vertical deviation, and vertical speed required) appear on the PFDs in magenta (Figure 6-11).
SECTION 6 – AUTOMATIC FLIGHT CONTROL When a descent leg is captured (Figure 6-12), Vertical Path Tracking becomes active and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.
SECTION 6 – AUTOMATIC FLIGHT CONTROL VNAV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile recapture.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture mode are armed in preparation to capture the new VNAV Target Altitude or the Selected Altitude, depending on which altitude is to be intercepted first.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Figure 6-16 Glidepath Mode Armed If vertical guidance becomes or is expected to become unavailable and the approach downgrades, Glidepath Mode is disarmed. When vertical guidance becomes available again, Glidepath Mode is automatically re-armed under GPS Approach Mode. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Roll Modes Go Around (GA) Mode Pushing the GA Switch engages the flight director in a wings level, 7° pitch-up attitude, allowing the execution of a missed approach or a go around. This mode is a both a pitch and roll mode and is annunciated as ‘GA’ in both the pitch and roll active mode fields. Go Around Mode disengages the autopilot and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the aircraft attitude (i.e.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Table 6-2 relates each roll mode to its respective control and annunciation. Refer to the pitch modes section for information regarding Go Around Mode. The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach modes. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS Button.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) Heading Select Mode is activated by pressing HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI. Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, BC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode. Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source on the HSI (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected navigation source.
SECTION 6 – AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.4 AUTOPILOT OPERATION NOTE: Refer to the AFM for specific instructions regarding emergency procedures. The autopilot operates flight control surface servos to provide automatic flight control. Pitch and roll commands are provided to the servos, based on the active flight director modes. The autopilot uses pitch and roll rates to stabilize the aircraft attitude during upsets and flight director maneuvers.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Disengaging the Autopilot Automatic disengagement occurs due to: • System failure • Inability to compute default flight director modes (FD also disengages automatically) • Invalid sensor data Automatic autopilot disengagement is indicated by a flashing red ‘AP’ annunciation and by the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC or MET Switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.5 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in this section are for instructional purposes only and should not be used for navigation. This section provides a scenario-based set of procedures showing various GFC 700 AFCS modes used while following a previously entered flight plan. The following example closely follows the example flight plan discussed in the GPS Navigation section.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure c) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode. Climbing to the Selected Altitude and flying an assigned heading: 1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob. 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). a) Adjust the vertical speed to the desired value.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan/GPS Course 2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS Navigation Mode, course changes defined by the flight plan are automatically made without pilot action required. NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Descent b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed automatically. While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV Target Altitude: • Press the VNV Key • Turn the ALT Knob to adjust the Selected Altitude 1) Select coupled VNAV: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT Knob, set the Selected Altitude at least 75 feet below the flight plan’s VNV Target Altitude of 10,000 feet.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Non-path descent using Flight Level Change Mode: The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 1) Command a non-path descent using Flight Level Change Mode: a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach KCOS Flying an ILS approach: PETEY 2 G HD e od M PYNON 1 GPS NAV Mode 2) Arm LOC Approach and Glideslope modes. a) Ensure the appropriate localizer frequency is tuned. b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. 3 LOC APR/ GS Mode 1) Transition from GPS Navigation Mode to Heading Select Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a WAAS precision approach: 2) Press the APR Key once clearance for approach has been acquired. GPS Approach Mode is activated and Glidepath Mode is armed. 4 CEGIX 3 GPS APR/ GP Mode 1) Arm flight director modes for a precision approach: a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around/Missed Approach Flying a missed approach: 1) Push the GA Switch at the Decision height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing yellow for 5 seconds and the autopilot disconnect aural alert.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Alerts The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Overspeed Protection Overspeed protection is provided in situations where the flight director cannot acquire and maintain the vertical Mode Reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed. When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The majority of the following discussions pertain to the Multi Function Display. In discussions pertaining to the PFD, the controls are located on the PFD. 7.1 NAVIGATION MAP PAGE WARNING: The map display should only be used for situational awareness. Any map display indication should be compared with approved navigation sources.
SECTION 7 – NAVIGATION 9) Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field. 10) Enter the desired target altitude offset from the selected Direct-to. 11) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘COURSE’ field. 12) Enter the desired course to the waypoint. Select a Direct-to Destination to a Nearest Airport 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left.
SECTION 7 – NAVIGATION 9) Turn the large FMS Knob to place the cursor in the ‘COURSE’ field. 10) Enter the desired course. 11) Press the ENT Key. The cursor now highlights ‘ACTIVATE?’. Figure 7-5 Recently Entered Waypoints List (MFD) 3) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints as shown in Figure 7-5. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to.
SECTION 7 – NAVIGATION Enter a Direct-to Destination 1) Press the Direct-to Key ( ). Select a Direct-to Destination to a Flight Plan Waypoint 2) Turn the large FMS Knob to place the cursor in the desired selection field. 1) While navigating an active flight plan, press the Direct-to ( ) Key. 3) Turn the small FMS Knob to begin selecting the desired identifier, location, etc. 2) Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7-8. 4) Press the ENT Key.
SECTION 7 – NAVIGATION 3) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position as shown in Figure 7-9. 2) Press the MENU Key to display the Options Window. The cursor will be flashing on ‘Cancel Direct-to NAV’. 4) Turn the large FMS Knob to select the desired airport. 3) Press the ENT Key to cancel the direct-to. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 7.3 6) Press ENT again to activate a Direct-to.
SECTION 7 – NAVIGATION 2) Figure 7-11 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight phase displayed on the HSI indicating 1.0 nm CDI scaling. 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 7-12. Note the current CDI flight phase is now ENR (Enroute).
SECTION 7 – NAVIGATION 4) V4 will now be entered into the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight the desired entry point as shown in Figure 7-13. The V4 entry will be placed immediately above the highlighted waypoint. Figure 7-14 Entering V4 Entry Point d) Press the ENT Key. TOP is now inserted into the flight plan as in Figure 7-15.
SECTION 7 – NAVIGATION f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as seen in Figure 7-17. j) Press the ENT Key. The selected airway and exit are displayed the prompt “LOAD?” highlighted as in Figure 7-18. Figure 7-16 List of Available Airways for TOP g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 7-16.
SECTION 7 – NAVIGATION Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 will now be made the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. c) Press the ACT LEG Softkey. The confirmation window is now displayed as in Figure 7-20. Note the TOP to SLN leg is actually part of V4.
SECTION 7 – NAVIGATION 6) The aircraft continues on heading 290º. When 2.0 nm from the intercept, the XTK will disappear from the HSI and the CDI will be positioned on the last dot indicating a 2.0 nm distance from the centerline of the next course. 8) At SLN, Victor Airway 244 (V244) will be intercepted. Turn prompts will be displayed in the PFD Navigation Status Box as seen in Figure 7-23. 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 7-22.
SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 will be intercepted. See Figure 7-25. Figure 7-26 Direct To OPSHN Figure 7-25 HYS to LAA Leg Active d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7-27. 11) ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and issues a crossing altitude restriction of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor.
SECTION 7 – NAVIGATION f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database, those altitudes will be displayed as white numerals. This indicates the altitudes will not be used by the system for vertical guidance until manually accepted by the pilot. To accept the displayed altitude, place the cursor over the altitude and press the ENT Key.
SECTION 7 – NAVIGATION b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7-31. e) Press the ENT Key. A list of available transitions for the selected approach is displayed as shown on Figure 7-32. Figure 7-30 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport will be displayed as in Figure 7-31.
SECTION 7 – NAVIGATION h) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values will always be displayed as white text, as in Figure 7-34.
SECTION 7 – NAVIGATION a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 7-35. b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to enter the desired value. 15) As seen in Figure 7-36, the aircraft is approaching TOD. Note the target vertical speed required to reach the selected altitude.
SECTION 7 – NAVIGATION 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-38. Keep Vertical Deviation Pointer Centered 18) The aircraft is approaching OPSHN. The upcoming turn and next heading will be annunciated at the top left of the PFD as seen in Figure 7-40. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
SECTION 7 – NAVIGATION 19) After passing OPSHN, the next leg of the arrival will turn magenta as shown in Figure 7-41. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-41 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 7-42).
SECTION 7 – NAVIGATION 21) Upon passing PYNON the approach procedure will automatically become active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-43). 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
SECTION 7 – NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-46) when the final approach course becomes active.
SECTION 7 – NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368FT’) is not part of the published procedure. It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach is exceeded.
SECTION 7 – NAVIGATION 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern will be established at the MAHP (MOGAL) as shown in Figure 7-49. 7.4 AIRPORT INFORMATION Figure 7-53 Airport Information Page Figure 7-49 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 750. Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION Select an Airport from the Active Flight Plan Select a Recently Entered Airport Identifier 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7-54. 2) Turn the small FMS Knob to the left.
SECTION 7 – NAVIGATION Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport. Continue turning the small FMS Knob to select the desired runway. 7.
SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-58 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1) With the NDB Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired selection field (identifier, name or closest city).
SECTION 7 – NAVIGATION 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.9 NEAREST AIRPORTS 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the flashing cursor. Access Runway Information for the Selected Airport 1) With the Nearest Airports Page displayed, press the RNWY Softkey to place the cursor in the ‘RUNWAYS’ field.
SECTION 7 – NAVIGATION Nearest Airports Information on the PFD Bearing TO 7.10 NEAREST INTERSECTIONS Distance Airport Symbol Identifier Runway Length Primary COM Frequency Figure 7-61 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports Window. View Information on a Specific Airport in the List 1) With the Nearest Airports Window displayed, turn either FMS Knob to place the cursor on the desired airport identifier.
SECTION 7 – NAVIGATION 7.11 NEAREST NDB 7.12 NEAREST VOR Figure 7-63 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon. Access Information on a Specific NDB 1) With the Nearest NDB Page displayed, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired NDB. The remaining information on the Nearest NDB Page pertains to the selected NDB.
SECTION 7 – NAVIGATION 3) Press the FMS Knob to remove the flashing cursor. 7.13 NEAREST USER WAYPOINT Figure 7-65 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the fifth rectangular page icon. Select a Nearest User Waypoint 7-28 3) Press the FMS Knob to remove the flashing cursor. 7.
SECTION 7 – NAVIGATION 7.15 NEAREST AIRSPACES View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ field. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor.
SECTION 7 – NAVIGATION Blank Page 7-30 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS 4) Repeat steps 2 and 3 until the desired name is entered. 5) Press the ENT Key. 6) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be modified by changing the reference waypoint. Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knobs to select a waypoint name. 5) Press the ENT Key to accept the selected name.
SECTION 8 – FLIGHT PLANNING turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. Figure 8-10 Create FPL on MFD Create a New Flight Plan Using the PFD NOTE: A flight plan cannot be entered using the PFD if another flight plan is active.
SECTION 8 – FLIGHT PLANNING 8.8 ENTER AN AIRWAY IN A FLIGHT PLAN 5) When the desired entry point is entered, press the ENT Key. 1) Press the FPL Key to display the active flight plan or display a stored flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the waypoint before which the airway will be entered. Figure 8-15 Airway Entry Point Loaded 6) Turn the small FMS Knob to display the Waypoint Information Window.
SECTION 8 – FLIGHT PLANNING 7) Press the LD AIRWY Softkey. A list of available airways is now displayed. 12) With ‘LOAD?’ highlighted, press the ENT Key. Figure 8-19 Airway Added to Flight Plan 8.9 Figure 8-17 Select Desired Airway 8) Turn either FMS Knob to highlight the desired airway. LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8.10 LOAD AN ARRIVAL 9) Press the ENT Key. A list of available exits is now displayed.
SECTION 8 – FLIGHT PLANNING 8.13 STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 8.15 DELETE A WAYPOINT FROM THE FLIGHT PLAN 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 1) With either the Active or Stored Flight Plan displayed, press the FMS Knob to activate the cursor. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan.
SECTION 8 – FLIGHT PLANNING 8.17 COPY A FLIGHT PLAN 1) From the Flight Plan Catalog press the FMS Knob to activate the cursor 2) Turn the large FMS Knob to highlight the flight plan to be copied. 3) Press the COPY Softkey. 4) A ‘Copy to flight plan #?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.
SECTION 8 – FLIGHT PLANNING 4) For Direct-to planning, press the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. Press the ENT Key and the flashing cursor moves to the ending waypoint field. Turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) If a flight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 9.2 APPROACHES NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. Figure 9-3 Select Arrival 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key.
SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a flight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 7) The cursor will move to the TRANSITIONS field.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ group to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic. 10.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Figure 10-5 Lightning Display Range Annunciation Select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1) With the Weather Group selected, press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’. 2) Turn the large FMS Knob to select ‘STRMSCP MODE’.
SECTION 10 – HAZARD AVOIDANCE 10.3 XM WEATHER (OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 1) Press the MAP Softkey. 2) Press the NEXRAD or XM LTNG Softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn the FMS Knobs to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – Pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • • • • Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 1200’ TNA Mute above & climbing, moving in the Traffic out of direction of the line Traffic Mode Status range NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group.
SECTION 10 – HAZARD AVOIDANCE 10.5 AVIDYNE® TAS600 SERIES Refer to the Avidyne® TAS600 Series Pilot’s Guide for a detailed discussion of the TAS system and an explanation of the aural alerts. Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. ‘OPERATING’ is displayed in the Traffic Mode field.
SECTION 10 – HAZARD AVOIDANCE 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the last rectangular page icon. 3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys.
SECTION 10 – HAZARD AVOIDANCE 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. NOTE: TAWS operation is only available when the G1000 is configured for a TAWS-B installation. Displaying Terrain on the TAWS Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS Page.
SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Red Terrain/Obstacle above or within 100’ below or above aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. ���������������������� ��������������������� ��������������� ������������������ ������ Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key.
SECTION 10 – HAZARD AVOIDANCE TAWS Inhibit Forward Looking Terrain Avoidance (FLTA) Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled. Inhibit TAWS: The Forward Looking Terrain Avoidance alert is composed of two sub-functions: While the TAWS Page is displayed, press the INHIBIT Softkey. ‘TAWS INHB’ will be annunciated in the lower right of portion of the screen.
SECTION 10 – HAZARD AVOIDANCE Premature Descent Alert (PDA) Excessive Descent Rate Alert (EDR) A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway. The PDA alert mode functions only during descent to land. PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.
��������������������������� SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map ���� ��� 1) With the Navigation Map displayed, press the MAP Softkey. ��� ��� ������������ ��� �� � ��� � ��� � ��� � ��� � ���� � ���� � ��� ��������������������������� �������������������� 2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 11 – ABNORMAL OPERATION 11.6 DEAD RECKONING While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position, the system will automatically revert to Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position.
SECTION 11 – ABNORMAL OPERATION will be disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) will be questionable. Finally, airspace alerts will continue to function, but with degraded accuracy. 11-4 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Airplane Flight Manual Supplement supersedes information found in this document. System Annunciation Red ‘X’ Annunciation Window Alerts Window Figure 12-1 G1000 Alerting System ALERTS Softkey Annunciation The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window displays abbreviated annunciation text.
SECTION 12 – ANNUNCIATIONS & ALERTS • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. Figure 12-2 WARNING Softkey Annunciation 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Diamond DA40 aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention. A warning alert is accompanied by an annunciation in the Annunciation Window.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA40 aircraft. See the Flight Manual Supplement for information regarding pilot responses. WARNING Alerts Annunciation Window Text OIL PRES LO FUEL PRES LO FUEL PRES HI ALTERNATOR STARTER ENGD DOOR OPEN TRIM FAIL Alerts Window Message Oil pressure is below 25 psi. Fuel pressure is below 14 psi. (1.0 psi on DA40F) Fuel pressure is greater than 35 psi. (8 psi on DA40F) Alternator failed.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 12-5 AFCS System Status Annunciation Condition Pitch Failure Roll Failure Roll axis control failure. AP is inoperative. AP TRIM Switch Stuck, or Pitch Trim Axis Control Failure System Failure If annunciated when AP is engaged, a failure has occurred in the pitch trim system.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.5 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment This annunciation will only be seen when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal flight parameter, possibly caused by strong turbulence. In this case, the situation should correct itself within a few seconds. If there is an actual failure, a red “X” will soon appear over the Attitude Indicator. Display system is not receiving airspeed input from air data computer.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.8 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section. NOTE: This section provides information regarding G1000 message advisories that may be displayed by the system.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message PFD1 KEYSTK – PFD1 [key name] Key is stuck. MFD1 KEYSTK – MFD [key name] Key is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage Comments A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. MFD1 DB ERR – MFD1 SafeTaxi database error exists. PFD1 DB ERR – PFD1 SafeTaxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. DB MISMATCH – Aviation database version mismatch. Xtalk is off.
SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Message GMA1 FAIL – GMA1 is inoperative. GMA1 CONFIG – GMA1 config error. Config service req’d. MANIFEST – GMA1 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. The audio panel configuration settings do not match backup configuration memory.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. MANIFEST – GIA1 software mismatch, communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch, be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments GPS NAV LOST – Loss of GPS Loss of GPS navigation due to position error. navigation. Position error. GPS NAV LOST – Loss of GPS Loss of GPS navigation due to GPS failure. navigation. GPS fail. ABORT APR – Loss of GPS navigation. Abort approach due to loss of GPS navigation. Abort approach. TRUE APR – True north approach.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories Message GIA1 CONFIG – GIA1 configuration error. Config service req’d. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced. GDL 69A Message Advisories Message GDL69 CONFIG – GDL 69 config error.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) TIMER EXPIRD – Timer has expired. DB CHANGE – Database changed. Verify user modified procedures. FPL TRUNC – Flight plan has been truncated. LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) PTK FAIL – Parallel track unavailable: IAF waypoint for parallel offset has been passed. past IAF. UNABLE V WPT – Can’t reach current The current vertical waypoint can not be reached within the maximum flight path vertical waypoint. angle and vertical speed constraints. The system will automatically transition to the next vertical waypoint. VNV – Unavailable.
SECTION 12 – ANNUNCIATIONS & ALERTS Blank Page 12-22 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-6, 1-7, 4-3 ADVISORY 12-1 Advisory alerts 12-3 AFCS 1-3, 6-1, 6-2, 6-23, 12-4 Age 10-6 AHRS 12-18, 12-19 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-25 Airport information 7-21 Airspace alerts 7-29 Airspeed indicator 2-3 Airspeed Reference 6-8 Airspeed trend vector 2-3 Airways 8-5 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-14 ALT 1-4, 1-7, 2-4, 6-4, 6-6, 6-13, 7-19 Altitude alerting 2-4
INDEX G GA 6-1 Glidepath 2-6, 7-19 Glidepath Mode 6-14, 6-20 Glidepath Mode (GP) 6-31 Glideslope 2-6, 7-19 Glideslope Mode 6-15, 6-20, 6-30 Glidesope Indicator 2-2 GMA 1347 1-1 Go Around 6-1 Go Around Mode 6-32–6-33 Go Around Mode (GA) 6-16 H Heading indication 2-9 Heading Select 1-3, 1-4 Heading Select Mode 6-18 Heading Select Mode (HDG) 6-24 Headset(s) 5-2 Horizontal situation indicator 2-8 HSI 2-8 Hurricanes 10-5 I ID 1-3, 4-3, 4-6 IDENT function 4-6 ILS approach 6-30 Imminent Terrain Impact 10-12 Impa
INDEX Roll Hold Mode (ROL) 6-17 Roll modes, flight director 6-16–6-19 Roll Reference 6-17 RTC 10-12 RVSI 7-15, 7-16 RX indicator 4-3 R indication 4-5 S U Unlighted obstacle 10-14 Secure Digital (SD) card 1-12 Selected Altitude 6-6, 6-10, 6-13 Selected Altitude Capture Mode 6-6, 6-10, 6-13 Selected Course 6-20 Selected Heading 6-18 Selected vertical speed 2-7 Servos 6-21 Severe thunderstorm 10-5 SIGMET 10-5 Slip/Skid indicator 2-3 Softkey function (MFD) 1-5, 1-8 Speed ranges 2-3 SQ 1-3 Squelch 5-3 STBY Sof
INDEX Weather product symbol 10-5 Weather product symbols 10-6 Weather warnings 10-5 Wind direction 10-5 Wind speed 10-5 Wings level 6-16, 6-17 X XPDR Softkey 4-4 Index-4 Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev.
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd Liberty House Hounsdown Business Park Southampton, SO40 9RB, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00324-07 Rev. A © 2004-2007 Garmin Ltd.
